Cathodic protection monitoring system

ABSTRACT

A cathodic protection (CP) interruption system includes a metallic structure and a plurality of passive CP units embedded in an electrolytic medium, a plurality of test units electrically coupled with the structure and each of the CP units, and a low-power consumption component arrangement. The arrangement includes a real-time clock (RTC) and a GPS receiver coupled with each test unit for receiving GPS time from a GPS satellite. A controller is communicatively coupled with each RTC and GPS receiver for activating the GPS receiver once the RTC reaches a predetermined time to synchronize a RTC time of each RTC with GPS time. Interruption modules are coupled in electrical and data communication with the controller. The controller selectively changes an activation state of each interruption module once the RTC time reaches a predetermined activation state change time to selectively electrically couple or decouple each CP unit from the structure.

FIELD

The present invention relates to cathodic protection systems and morespecifically to monitoring cathodic protection systems for metallicstructures embedded in electrolytic media.

BACKGROUND

Metallic objects embedded in electrolytic media are generally subject tocorrosion. Corrosion is a natural process which converts a refined metalinto a more chemically stable form such as an oxide, hydroxide orsulfide. Corrosion is a deterioration and destruction of the materialmaking up the metallic object and is caused by electrochemical reactionsbetween the material making up the metallic object and its electrolyticmedia environment. Moisture, material composition, pH, temperature andpolarization are some of the factors which may influence the rate ofcorrosion of the metallic structure.

Metallic objects such as pipelines embedded in electrolytic media suchas soil are subject to corrosive electrochemical forces. Pipelinecorrosion can result in damage, which is costly to repair, and which ispotentially hazardous to the operation of the pipeline itself. Corrodedpipelines can be subject to failure or contamination which can result inrelease of potentially hazardous materials into the natural environment.

Galvanic corrosion occurs on pipelines when two different metals areplaced in physical or electrical contact with each other and areimmersed in the soil. The more active metal, called the “anode”,corrodes at a faster rate and the more stable metal, called the“cathode”, corrodes at a slower rate.

One method for protecting against pipeline corrosion includes cathodicprotection. Cathodic protection (CP) makes the metal structure to beprotected, in this case the pipeline, the cathode of an electrochemicalcell. This may be done, for example, by connecting the pipeline to ametal object or structure which is more easily corroded to act as theanode of the electrochemical cell. Thereby, the more easily corrodedmetal becomes a “sacrificial anode”. Galvanic sacrificial anodes may bemade, for example, from Zinc, Magnesium or Aluminum. These types ofsystems are known as “passive systems”.

In “impressed current” systems, the cathodic protection system mayinclude currents applied from an external power source, such as arectifier. The rectifier is connected to the pipeline and one or moreanodes. Current is passed from the rectifier to the pipeline to providecathodic protection. Electrons leaving the anode are received by therectifier. This reduces or eliminates consumption of the anodes in thecathodic protection system. A plurality of cathodic protectionrectifiers to be located along the pipeline to apply a protectioncurrent there along. Rectifiers in impressed current systems may drawtheir power from line power, solar panels, wind generators, batteriesfor storing energy therefrom, or thermoelectric generators, to name afew. Rectifier systems which use batteries typically rely on anotherpower source, such as solar panels, to “top up” the battery as it isdepleted.

Between the passive cathodic protection systems and the impressedcurrent cathodic protection systems, the passive cathodic protectionsystems, or galvanic protection, are easier to install, tend to be morecost-effective and are more energy efficient as they do not requireexternal power.

To provide consistent protection, the electrochemical exchange betweencathode and anode, or the pipeline structure and the cathodic protectionsystem, must be maintained in balance. Over-application of cathodicprotection can result in damage to pipeline coatings or hydrogenembrittlement, for example. Too little protection and the pipelinestructure will still be subject to corrosion. Accordingly, once they arein place, the level of cathodic protection must be periodically testedto monitor performance of the cathodic protection system.

Methods for assessing the performance of the cathodic protection systeminclude obtaining measurements of potential between the cathodicallyprotected pipeline metal structure and a reference electrode. Thisallows for measurement of the “pipe-to-soil” potential, which is thepotential difference generated between the pipeline and its surroundingsoil. This potential difference is the result of electrolytic action anda cause of corrosion of the pipeline. Accordingly, pipe-to-soilpotential is important for evaluating the corrosive conditions of theenvironment or for evaluating the extent of cathodic protection beingapplied.

One tool for assessing the performance of a cathodic protection systemis a reference electrode. A reference electrode, or “half-cell” is astable electrode having known potential. The purpose of a referenceelectrode is to allow for determination of the potential of the otherelectrode or “half” of the electrochemical cell. One common type ofreference electrode is the copper/copper sulfate (CSE) electrode.

Pipe-to-soil potential is typically measured at one or more teststations along the pipeline. Each test station is electrically connectedto the pipeline by a test cable. Thereby, the potential of the pipelinemay be measured from the test station. The reference electrode may beplaced in the soil in the vicinity of the protected pipeline. Avoltmeter is connected between the test station and the referenceelectrode, with its negative terminal connected to the terminal of thereference electrode and the positive terminal connected to the teststation. Thereby, a galvanic cell is created by connecting the two“half-cells” together, the first half being the natural half-cellsformed between the pipeline and the soil and the second half-cell beingthe reference electrode. Accordingly, the voltage between the buriedpipeline and the surrounding soil, or pipe-to-soil potential, may bemeasured.

However, in some environments, measuring pipe-to-soil potentialaccurately can be challenged by other currents in the soil. Sources ofsuch other currents include nearby electric trains, other cathodicprotection systems, power lines, welding or telluric current, forexample. Accordingly, it is beneficial to electrically isolate thecathode or pipeline just prior to measuring the pipe-to-soil potential.

One tool for electrically isolating the cathode at the time ofpipe-to-soil potential measurement is the cathodic protection (CP)coupon. A CP coupon can also be used to determine the corrosion rate ofthe material making up the pipeline. Coupons are an uncoated sample ofthe same material used to fabricate the pipeline and are typicallyweighed and measured prior to burial adjacent to the pipeline structure.The coupon is electrically connected to the pipeline by wire, forexample. The coupon simulates an uncoated portion of the pipeline alsoknown as a “holiday”.

For monitoring of cathodic protection potential, the connection betweenthe coupon and the pipeline structure is instantaneously interrupted oris interrupted nearly-instantaneously. Similarly, the referenceelectrode is preferably placed in a tube to eliminate any potential dropin the soil during measurement. Thereby, the polarized potential of thecoupon can be measured with respect to the reference electrode placed inthe tube. If the polarized potential of the coupon is indicative ofadequate cathodic protection, then any unprotected pipeline structure ofthe same size or smaller should be equally protected.

The use of CP coupons for measuring pipe-to-soil potential is beneficialas the potential of the pipeline structure can be inferred from thecoupon, adequate cathodic protection can be confirmed without the needto interrupt all sources of current in the vicinity of the pipeline,readings will be free of potential drop and can also be used to detecthazardous voltages.

Corrosion is unlikely where a measured AC current density of the couponis 0 to 20 A/m2. AC corrosion is unpredictable where the AC currentdensity is 20 A/m2 to 100 A/m2 and is likely at greater than 100 A/m2.

The cathodic protection monitoring system is deployed at various pointsin preferably all along the pipeline and related structures.Accordingly, the cathodic protection monitoring system includes aplurality of test stations. Due to the length of pipelines, which canstretch hundreds of kilometers, the test stations are geographicallydispersed. It is preferable to take measurements at each test stationsimultaneously. Accordingly, the interruption of the circuit between theburied coupon in the cathodic protection system must be synchronized ateach station. Previous systems which rely on such synchronizationtypically have sources of external power. Such as impressed currentrectifier systems for example. However, there is a desire to provide apassive system which provides the advantages associated withsynchronized interruption along with reduced demands for power.

SUMMARY

The present invention relates to cathodic protection systems and morespecifically to monitoring cathodic protection systems for metallicstructures embedded in electrolytic media.

Cathodic protection may be applied to a variety of suitable metallicstructures. Metallic structures suitable for cathodic protection systemas described herein may include, by way of non-limiting example, marinestructures, storage tanks, bridges, power line towers or otherelectrical grid infrastructure and pipelines for conveying fluids suchas oil, water or gas. Accordingly, the electrolytic media may also takea variety of suitable forms depending on the environment within whichthe metallic structure resides. The cathodic protection system isdescribed herein within the context of a preferred aspect wherein themetallic structure is a pipeline, such as an oil pipeline, and theelectrolytic media is soil within which the pipeline is embedded.However, it should be understood that the present invention is notlimited to this preferred aspect and may be applicable to other metallicstructures is other electrolytic media environments.

In one aspect, there is provided a cathodic protection interruptionsystem including a metallic structure embedded in an electrolyticmedium, a plurality of passive cathodic protection units embedded in theelectrolytic medium adjacent to and spaced apart along the metallicstructure, a plurality of test units electrically coupled with themetallic structure and each of the plurality of passive cathodicprotection units, and, a low-power consumption component arrangement.The low-power consumption component arrangement includes a localreal-time clock coupled with each test unit of the plurality of testunits and a global positioning system (GPS) receiver coupled with eachtest unit of the plurality of test units for receiving GPS time from atleast one global positioning system satellite in data communicationtherewith. The low-power consumption component arrangement furtherincludes at least one controller communicatively coupled with eachreal-time clock and each GPS receiver for activating the GPS receiveronce the local real-time clock reaches a predetermined real-time clocktime to synchronize a real-time clock time of each local real-time clockwith GPS time, and, a plurality of interruption modules each coupled inelectrical and data communication with the at least one controller. Theat least one controller may selectively change an activation state ofeach interruption module of the plurality of interruption modules oncethe real-time clock time reaches a predetermined activation state changetime to selectively electrically couple or electrically decouple eachpassive cathodic protection unit of the plurality of passive cathodicprotection units from the metallic structure. In one aspect, thereal-time clock is a digital temperature-compensated crystal oscillator(DTCXO). Ones of the passive cathodic protection units of the pluralityof passive cathodic protection units are selected from the groupconsisting of bonds and sacrificial anodes. The GPS receiver may bedeactivated after synchronization until the real-time clock reaches thepredetermined real-time clock time. In one aspect, a local power sourcemay be electrically coupled with at least one of the test stations andthe interruption module. The local power source may be a battery absentexternal augmentation

The metallic structure may be one of a pipeline, a marine structure, astorage tank, a bridge, a power line tower, an electrical gridinfrastructure component and a coupon. The electrolytic medium is atleast one of soil and water.

A plurality of reference electrodes may each be embedded in theelectrolytic medium proximate to the metallic structure and electricallycoupled with a corresponding test unit of the plurality of test units.The system may include a plurality of voltmeters wherein one voltmeterof the plurality of voltmeters is electrically coupled between eachreference electrode and corresponding test unit of the plurality of testunits.

The system may include a plurality of remote monitoring units eachhousing a corresponding one of the at least one interruption modules andin electrical communication and data communication with a correspondingtest unit of the plurality of test units. Each remote monitoring unit ofthe plurality of remote monitoring units may be configured for wirelesscellular communication or may be configured for wireless satellitecommunication. A battery may serve as a sole power source for at leastone of the remote monitoring unit and the corresponding test station.The battery may be absent connection with an external power source.

At least one low earth orbit L-band satellite may be in datacommunication with each remote monitoring unit of the plurality ofremote monitoring units.

In another aspect, at least one coupon may be embedded in theelectrolytic medium adjacent the metallic structure and electricallycoupled with the at least one cathodic protection unit via the teststation. A switch may be electrically coupled between the at least onecoupon and the test station for selectively coupling and decoupling theat least one coupon from the at least one cathodic protection unit.

In another aspect, there is provided a cathodic protection interruptionsystem including a metallic structure embedded in an electrolyticmedium, at least one passive cathodic protection unit embedded in theelectrolytic medium adjacent to the metallic structure, a test unitelectrically coupled with the metallic structure and the passivecathodic protection unit, and a low-power consumption componentarrangement. The low-power consumption component arrangement includes alocal real-time clock coupled with the test unit and a globalpositioning system (GPS) receiver coupled with the test unit forreceiving GPS time from at least one global positioning system satellitein data communication therewith, at least one controller communicativelycoupled with the real-time clock and the GPS receiver for activating theGPS receiver once the local real-time clock reaches a predeterminedlocal time to synchronize the local real-time clock with GPS time, andan interruption module coupled in electrical and data communication withthe at least one controller. The at least one controller may selectivelychange an activation state of the interruption module once the real-timeclock time has reached a predetermined activation state change time toselectively electrically couple or electrically decouple the passivecathodic protection unit from the metallic structure.

In another aspect there is provided a method for changing an activationstate of an interruption module for selectively interrupting at leastone passive cathodic protection unit from a metallic structure. Themethod includes the steps of enabling a global positioning system (GPS)receiver in data communication with a controller of the interruptionmodule, receiving GPS time via the GPS receiver from at least one globalpositioning system satellite in data communication therewith,synchronizing a real-time clock time of a real-time clock in datacommunication with the controller to GPS time, disabling the GPSreceiver and changing the activation state of the interruption module ifa predetermined activation state change time of the interruption moduleis between the local real-time clock time and the GPS time. The methodmay further include the step of enabling the GPS receiver upon expiry ofthe predetermined time period.

The step of disabling the GPS receiver may further include disabling theGPS receiver for a predetermined time period.

The step of synchronizing the real-time clock with GPS time may furtherinclude synchronizing the real-time clock with GPS time when thereal-time clock leads GPS time.

In one aspect, the predetermined activation state change time may be apredetermined activation time and the interruption module may beactivated at the step of changing the activation state. In anotheraspect, the predetermined activation state change time may be apredetermined de-activation time and the interruption module isde-activated at the step of changing the activation state.

In another aspect, prior to the step of receiving GPS time via the GPSreceiver, the method may further include the step of establishing a datacommunication lock between the GPC receiver and the at least one globalpositioning system satellite.

The metallic structure may be one of a pipeline, a marine structure, astorage tank, a bridge, a power line tower, an electrical gridinfrastructure component and a coupon. In one aspect, the metallicstructure is a coupon which is embedded in the electrolytic mediumadjacent the pipeline and electrically coupled with the passive cathodicprotection unit via a switch electrically coupled between the coupon andthe test station for selectively coupling and decoupling the at leastone coupon from the passive cathodic protection unit.

BRIEF DESCRIPTION OF THE DRAWINGS

FIG. 1 illustrates a cathodic protection system in accordance withembodiments of the present invention;

FIG. 2 illustrates a cathodic protection system using a coupon;

FIG. 3 illustrates a rectifier coupled with a test station and areference electrode;

FIG. 4 illustrates a reference electrode;

FIG. 5 illustrates the interruption module of the remote monitoringunit;

FIG. 6 illustrates a synchronization method between the GPS satellitesystem and the Real Time Clock of the remote monitoring unit of FIG. 5;

FIG. 7 illustrates the operation of the interruption module of FIG. 5;

FIG. 8 illustrates communications system which may be used withembodiments of the invention; and,

FIG. 9 illustrates a Global Positioning System (GPS) Satellite systemfor use with one embodiment of the invention.

DETAILED DESCRIPTION

The present invention relates to cathodic protection systems and morespecifically to monitoring cathodic protection systems for metallicstructures embedded in electrolytic media.

Cathodic protection may be applied to a variety of suitable metallicstructures. Metallic structures suitable for cathodic protection systemas described herein may include, by way of non-limiting example, marinestructures, storage tanks, bridges, power line towers or otherelectrical grid infrastructure and pipelines for conveying fluids suchas oil, water or gas. Accordingly, the electrolytic media may also takea variety of suitable forms depending on the environment within whichthe metallic structure resides. The cathodic protection system isdescribed herein within the context of a preferred aspect wherein themetallic structure is a pipeline, such as an oil pipeline, and theelectrolytic media is soil within which the pipeline is embedded.However, it should be understood that the present invention is notlimited to this preferred aspect and may be applicable to other metallicstructures is other electrolytic media environments.

With reference to the aspect illustrated in FIG. 1, there is shown amonitoring system 10 for monitoring a cathodic protection (CP) system 16for applying cathodic protection to a structure embedded or buried in anelectrolytic medium, such as a pipeline 14 buried in soil 12. To providecathodic protection to the pipeline 14, the cathodic protection system16 may include one or more passive cathodic protection units such as oneor more sacrificial galvanic anodes 18 embedded in the soil 12 adjacentthe pipeline 14 and spaced apart there along. With respect tosacrificial anodes, a metal which is more reactive than the metal makingup the pipeline 14 is connected to the pipeline 14. The more reactivemetal makes up the anode of an electrochemical cell and the pipeline 14makes up the cathode of the electrochemical cell. Thereby, thesacrificial anode 18 is consumed and the pipeline 14 is protected fromcorrosion.

In another aspect, the cathodic protection system 16 may providecathodic protection to the pipeline 14 via passive cathodic protectionunits such as one or more bonds 20. Cathodic protection systems instructures adjacent the pipeline 14 may interfere electrically with thecathodic protection of the pipeline 14. Currents produced within theenvironment by other cathodic protection systems can flow between thepipeline 14 and other secondary structures, such as the secondarypipeline 22. To control such currents, the pipeline 14 may be bonded byelectrical connection to the secondary structure, in this case secondarypipeline 22. Such bonding balances the potential difference between theprimary pipeline structure 14 and the secondary pipeline structure 22and also controls the path of stray currents. Bonding not only providesfor corrosion protection, but also reduces interference of measurementsmade while testing or monitoring cathodic protection system 16.

It should be understood that bonds 20 and sacrificial galvanic anodes 18may be used contemporaneously on the same pipeline structure orsuitability may determine which means for cathodic protection isdeployed.

The monitoring system 10 may also include at least one above groundtesting station 24 electrically coupled to the pipeline 14 and cathodicprotection system 16, including the galvanic anode 18 or the bondedsecondary structure 22 as the case may be. The testing stations 24 arealso electrically coupled with a reference electrode 26 which will bediscussed in further detail hereinafter.

Each testing station 24 may have coupled thereto a remote monitoringunit (RMU) 28 which is in electrical communication and datacommunication therewith. The testing station 24 is also configured forautomated testing and monitoring of the cathodic protection applied tothe pipeline 14 at various locations, some of which may begeographically remote and/or difficult to access by personnel forin-person testing and monitoring. The remote monitoring unit 28 providesfor storage of data obtained from the testing station 24 and alsoprovides for transmission of the data to a remote location and receptionof information and commands from a remote location as will also bediscussed further hereinafter.

As shown in FIG. 2, the monitoring system 10 may include a coupon 30adjacent the pipeline 14. A coupon is typically an uncoated piece of thematerial used to make up the pipeline 14. The coupon 30 simulates a barespot or “holiday” of similar size on the pipeline 14. Coupon 30 is usedfor measurement of the performance of the cathodic protection system 16.Coupon 30 is selectively in electrical connection with the pipeline 14via a switch 32 within the testing unit 24 for interrupting theconnection between the coupon 30 and the cathodic protection system 16coupled with the pipeline 14.

Test stations 24 are preferably placed at regular intervals along thepipeline 14 for testing corrosion severity along the pipeline 14. Eachtest station 24 is configured to read pipe-to-soil potentials orvoltages with the use of coupon 30 and a reference electrode 26, whichis preferably embedded in close proximity of pipeline 14, as shown inFIG. 3. Reference cell 26 is used as one half of an electrochemicalcell, in this instance the anode, to determine the cell potential of theother half of the electrochemical cell, in this case the cathode. Whenmeasuring the potential, coupon 30 is electrically disconnected from thepipeline 14 via switch 32, and so coupon 30 forms an electrochemicalcell with reference electrode 26. Pipe-to-soil potential is the voltagepotential generated between the buried pipeline 14 and its surroundingsoil 12 and is a cause of electrolytic corrosion of the pipeline 14.Accordingly, measurements of pipe-to-soil potential difference takenusing the coupon 30 and the reference electrode 26 provide a measurementof the severity of corrosive activity along the pipeline 14.

FIG. 4 illustrates reference electrode 26 in further detail. Thereference electrode 26 includes a tube or can 37 within which is amaterial 39 having a known electrode potential. At a first end portion41 thereof, the tube 37 is plugged by plug 43 which is preferably of aporous material. At a second end portion 45 thereof, the tube 37 has acap 47 which is preferably removable for selectively closing and openingthe tube 37. Extending from the cap 47 into the tube 37 is a rod 49which is preferably composed of a pure, electrically conductivematerial. There is also provided a connection 51 for connection to thetesting station 24. Connection 51 is electrically connected with the rod49 through an aperture (not shown) in the cap 47. Tube 37 may also havean inspection window 53 so that the interior of the tube 36 may beobserved from the exterior, if desired.

With reference to FIG. 5, there is shown the primary controller 34 ofthe testing unit 24 coupled with an interruption module 38, orinterrupter, of remote monitoring unit 28 via a bus 40 facilitating theexchange of at least one of power and data between the interruptionmodule 38 and the primary controller 34. The primary controller 34 ofeach testing unit include any number or combination of controllers,processors, circuits, integrated circuits, programmable logic devices,microcontrollers, or other suitable controlling devices and any local orexternal memory for storing data and other information accessed orgenerated by the testing unit 24.

The primary controller 34 of the testing unit 24 includes a multiplexer42 electrically connected with the reference electrode 26, the pipeline14, the coupon 30, a native/AC coupon, and any bonds 20 between primarystructure 14 and secondary structures 22. The multiplexer 42 receivesanalog inputs from one or more of the aforementioned components viamultiplexer input connections 44 and selects between these input signalsand forwards them to output lines 46. Signals output from multiplexer 42pass through an amplifier 48 and then to an analog-to-digital converter(ADC) 50. Signals passing from the amplifier 48 to ADC 50 may first passthrough a root mean square (RMS) voltage circuit 52. RMS circuit 52 is ameans for providing an AC sine wave form as an equivalent voltage whichrepresents the corresponding DC voltage that would produce the sameeffect downstream. Once the analog signals are received and converted todigital signals by ADC 50, the digital signals are output via outputline 54 to the central processing unit (CPU) or central controllermodule 56.

CPU 56 is also coupled with a transceiver 58, a GPS receiver 60, areal-time clock (RTC) 62 and a display 64. Transceiver 58 is preferablya wireless transceiver for satellite or cellular communication withother test units, or a Web server or host computer as will be describedfurther hereinafter. GPS receiver 60 is capable of receiving informationfrom satellites and calculating the geographic position of the testingunit 24 based on the received satellite signals. Such communication withthe GPS receiver 60 is facilitated by a radio frequency antenna device70. Real-time clock 62 may be any suitable real-time clock and iscoupled with CPU 56 to control when power is provided components of thetesting unit 24, or when signals are to be sent by the transceiver 58,or to synchronize with the interruption module 38 when measurements areprogrammed to be taken, as will be described further hereinafter.Preferably, RTC 62 is a digital temperature compensated Crystaloscillator (DTCXO), which is a type of RTC module having a crystal whichoscillates at 32.768 kHz. Advantage is provided by DTCXO RTCs becausethey have built-in temperature compensation circuitry and also featurelow power consumption. RTC 62 is preferably coupled with a second radiofrequency antenna device 72. Display 64 provides for display of datareceived, collected or determined by operation of the testing unit 24.The primary controller 34 also includes a power source 66, such as abattery electrically coupled with a system power regulator 68.

The interruption module 38 includes a multiplexer 74 electricallyconnected with the reference electrode 26, primary structure or pipeline14 and secondary structure 22, such as secondary pipeline 22. Themultiplexer 74 of interruption module 38 may also be electricallyconnected a bond circuit 76, which may include a positive bond terminal78, negative bond terminal 80 and a shunt resistor 82 electricallyconnected between the positive bond terminal 78 and the negative bondterminal 80. The multiplexer 74 receives analog inputs from one or moreof the aforementioned components via multiplexer input connections 84and selects between these input signals and forwards them to outputlines 86. Signals output from multiplexer 74 pass through an amplifier88 and then to an analog-to-digital converter (ADC) 90. Signals passingfrom the amplifier 88 to ADC 90 may first pass through a root meansquare (RMS) voltage circuit 92. Once the analog signals are receivedand converted to digital signals by ADC 90, digital signals are outputvia the output line 94 to the central processing unit (CPU) or centralcontroller module 96 of the interruption module 38.

CPU 96 is also coupled with a real-time clock (RTC) 98 and a display100.

Real-time clock 98 may be any suitable real-time clock and is coupledwith CPU 96 to control when power is provided components of the remotemonitoring unit 28, or to synchronize with the primary controller 34when measurements are programmed to be taken, as will be describedfurther hereinafter. Preferably, RTC 98 is a digital temperaturecompensated Crystal oscillator (DTCXO). Display 100 provides for displayof data received, collected or determined by operation of the remotemonitoring unit 28. The interruption module 38 also includes a powersource 102, such as a battery electrically coupled with a system powerregulator 104.

The power source and system power regulator of the interruption moduleare electrically coupled with the power source 66 and system powerregulator 68 of the primary controller 34 via the bus 40. Similarly, CPUis coupled unit data communication with CPU 56 of the primary controller34 via bus 40.

When used in an arrangement wherein there is a bond circuit 76 betweenthe primary structure 14 and secondary structure 22, the interruptionmodule 38 typically measures the DC potential of the protected structure14 relative to the reference electrode 26, the AC potential of theprotected structure 14 relative to the reference electrode 26, the DCpotential of the secondary structure 22 relative to the referenceelectrode 26, the AC potential of the secondary structure 22 relative tothe reference electrode 26, the DC current flow between the secondarystructure 22 and the protected structure 14, the AC current flow betweenthe secondary structure 22 and the protected structure 14 and theinstant disconnect potential on the protected structure 14 relative tothe reference electrode 26. This last measurement is made a programmableamount of time after the interruption relay opens and the bond circuit76 is disconnected.

Used in an arrangement wherein there is a galvanic anode 18 electricallycoupled with the primary structure 14, the interruption module 38typically measures the DC potential of the protected structure 14relative to reference electrode 26, the AC potential of the protectedstructure 14 relative to the reference electrode 26, the DC potential ofthe galvanic anode 18 relative to the reference electrode 26, the ACpotential of the galvanic anode 18 relative to the reference electrode26, DC current flow between the galvanic anode 18 and the protectedstructure 14, AC current flow between the galvanic anode 18 and theprotected structure 14, in the instant disconnect see potential on theprotected structure 14 relative to the reference electrode 26. This lastmeasurement is made a programmable amount of time after the interruptionrelay opens and the galvanic anode 18 is disconnected.

FIG. 6 illustrates a method 600 for synchronizing GPS to the real-timeclock (RTC) 62 of the primary controller 34 of the test unit 24. Themethod 600 is initiated once the relay controlling the GPSsynchronization switches to the “ON” state. At step 602, GPS receiver 60is enabled. At step 604 check is performed to determine whether the GPSreceiver 60 has a lock on the time. The method will cycle through thisstep until the GPS receiver 60 has a time lock. Once the GPS receiver 60has a time lock, the method proceeds to step 606 where a check isperformed to determine whether the local RTC 62 leads the time receivedby GPS receiver 60. If yes, then the local RTC 62 is set to the GPS timeat step 608 and GPS receiver 60 is disabled at step 610. Once the GPSreceiver 60 is disabled, a check will be cycled until 30 minutes haveelapsed, as shown at step 612. Upon expiry of 30 minutes or more, themethod returns to step 602 and the GPS receiver 60 is once againenabled. Returning now to step 606, where the local RTC 62 does not leadthe GPS time obtained by the GPS receiver 60, the method then proceedsto step 614 whereupon a check is performed to determine whetherinterruption module 38 will transition to enable or disable interruptionrelay. If no, the method returns to step 608, where the local RTC timeis set to the GPS time. If yes, the method proceeds to step 616, whereina relay controlling the state of the interruption is flipped and themethod then proceeds back to step 608 wherein the local RTC timesynchronized with GPS time in step 610 wherein the GPS receiver isdisabled.

FIG. 7 illustrates a method 700 for driving the interruption relay. Themethod 700 is initiated once the relay controlling the interruptiondrive is switched to the “ON” state. The interruption peripheral 38 willwait until a signal is received from a central controlling server orfrom a local control device before it will enter interruption mode, aswill be described further hereinafter. Interruption mode comprisesseveral parameters, including the following:

1. Start date/time

2. End date/time

3. On phase duration

4. Off phase duration

5. Phase at top of minute

Once the signal with these parameters has been received and currentdate/time is between the start and end date/time, the remote monitoringunit 28 will enter interruption mode. At this point, the local real timeclock (RTC) counter will be aligned to GPS time by enabling the GPSreceiver 60 and waiting until a valid time is present on the GPSreceiver 60. The local RTC counter is set to the received GPS time andthe GPS receiver is turned off, in accordance with method 600 shown inFIG. 6.

At step 702 a check is performed to determine if the interruption modeis enabled. If interruption mode is not enabled, then the methodproceeds to step 704 wherein it is determined whether the interruptionrelay is switched to the “ON” state. If yes, then the method returns tostep 702. If no, then the method proceeds to step 706 wherein the relayis switched to the “ON” state, thereby changing the activation state ofthe interruption module relay. The method then returns to step 702.

While interruption mode is enabled, a waveform transition always occursat a predetermined point in time, which in this aspect is preferably thetop of the minute. The ON/OFF phase at the top of the minute isprogrammable through the signal from the central server or the localcontrol device. For each duration of the on phase and the off phase, therelay that connects the protected structure to either the bond or thegalvanic anode, as the case may be, is turned on or off accordingly. Ifthe sum of on and off durations does not allow for an integer number ofcycles in the period of one minute, the final phase before the top ofthe minute is shortened to allow a transition to occur again at the topof the minute.

This is illustrated in FIG. 7, wherein the method proceeds from step 702to step 708 wherein the “ON” time (T2) and the “OFF” time (T3) are set.The method then proceeds to step 710 wherein a check is performed toensure that the interruption mode is enabled. If no, then the methodreturns to step 706 to change the relay activation state and set theinterruption relay to “ON”. If yes, then the method proceeds to step 712wherein it is determined if T2 has expired. If yes, then the methodproceeds to step 714 wherein the activation state is changed and therelay is set to “ON” and T2 is reset and the method returns to step 710.If T2 has not expired, the method proceeds to step 716 it is determinedif T3 has expired. If yes, then the method proceeds to step 718 whereinthe activation state is changed and the interruption relay is set to“OFF” and T3 is reset and the method returns to step 710. If T3 has notexpired, then the method proceeds from step 716 to step 710 directly todetermine if interruption mode is enabled.

Also, while interruption mode is enabled, the GPS receiver 60 will beturned on periodically (1-30 minutes) and allowed to lock onto GPS timefrom the GPS satellite constellation, in accordance with method 600shown in FIG. 6. Once lock is achieved, the local RTC counter is updatedand adjustments are made to the interruption relay activation state asneeded. The GPS receiver 60 is then turned off again. Keeping the GPSreceiver off for most of time during the interruption mode allowssignificant power savings. In a preferred aspect, the period at whichthe GPS receiver 60 is turned on periodically is determined by themaximum allowable drift, as determined by the application, of the timein local RTC 62 relative to UTC time. Once the end date/time T3 isachieved the unit will turn the relay on and stop the interruptioncycling. It should be understood that the interruption mode may also becanceled where a subsequent signal is received from the central serveror the local control device cancelling the interruption mode.

As the remote monitoring unit 28 and interruption module 38 arepreferably battery operated and more preferably powered only by abattery which is not connected with an external augment or power sourcesuch as grid power or solar power. Accordingly, it is advantageous toreduce the power consumption of these devices. It is thereforepreferable to rely on an Iridium low Earth orbit L-band satellite systemor other such low Earth orbit L-band satellite systems that may existnow or in the future. Such a system, shown in FIG. 8 enables powersavings to facilitate achievement of longer battery life.

The power required to send a signal from one point to another point in aradio system is governed by the Friis transmission formula:

$P_{R} = \frac{P_{T}G_{T}G_{R}c^{2}}{\left( {4\pi\;{Rf}} \right)^{2}}$Where P_(R) = Power  received P_(T) = Power  transmittedG_(T) = Gain  of  transmitting  antennaG_(R) = Gain  of  receiving  antenna c = Speed  of  lightR = Distance  between  transmitter  and  receiver  antennasf = Frequency  of  radio  signal  being  transmitted

It is apparent from this equation that link power loss is proportionalto both distance and frequency squared. For a given signal modulation, aminimum signal level is required for the signal to be deportable by thereceiver. If the gains of the antennae are maintained either or both ofthe frequency and distance are increased, and to maintain minimum signallevel at the receiver, transmission power must be increased tocompensate. Since the link power loss is proportional to the square ofthe distance and frequency, any increase in either parameter requiresthat the transmit power be substantially increased to make up thedifference.

In the case of Iridium low Earth orbit L-band satellites, distance issmall as compared to other satellite systems. While L-band is also usedwith some geostationary satellite systems, distance of the Iridiumsatellites is 780 km, while the distance to geostationary satellites isapproximately 35,786 km. The distance is therefore 45.8 times furthergeostationary satellites over low-Earth orbit satellites and requires2105 times (33.23 dB) more power to transmit to a geostationarysatellite as compared to the low-Earth orbit satellite. Similarly, whileother low Earth orbit satellite systems do exist, most do not useL-band. Iridium operates at approximately 1625 MHz, while otherconstellations operate in Ka (26.5 to 40 GHz) or Ku (12 to 18 GHz)bands. Even at the lowest frequency of Ku, 54.5 times (17.37 dB) as muchpower must be transmitted to make up for the loss due to the higherfrequency of Ku over L-band.

While some of the link margin lost could be made up with directionalantenna, several problems exist with that solution. First, the antennaewill no longer fit inside a small compact product as a directionalantenna requires a much larger footprint than a wide beam. Second, forgeostationary satellites, precision aiming of the antenna would berequired, which would make for a difficult product installation.Finally, for low Earth orbit constellations, the positions of satellitesoverhead are constantly changing, which would require that a beamsteering mechanism be present, whether mechanical or electronic, both ofwhich require space and power.

The Iridium low Earth orbit L-band system has both favorable parametersrequired for low-power operation and compact antennas. This provides forminimal distance between the ground transceiver and the satellites andlow-frequency operation.

With reference to FIG. 8, there is shown a system 106 for communicationbetween the primary controller 34 or interruption module 38 and asatellite ground station 108. In this aspect, satellite ground station108 is capable of transmitting and receiving signals to and fromsatellite 110, as discussed above, satellite 110 is preferably a L-bandlow Earth orbit satellite which requires a signal frequency ofapproximately 1625 MHz. Satellite 110 is capable of transmitting andreceiving signals to and from primary controller 34 and/or theinterruption module 38. Satellite ground station 108 is also incommunication with any suitable computer or processor, such as computer112, any suitable mobile device 114 or any data center or server 116.Such devices may communicate with the satellite ground station 108 overany suitable network, such as the Internet 118.

In accordance with another aspect, the primary controller 34 and/orinterruption device 38 may communicate with the computer 112, mobiledevice 114 or server 116 by way of a cellular communication system 120.The cellular communication system 120 may be connected with the devicesvia any suitable communication network, such as the Internet 118.

The aforementioned components and method steps, combined as describedherein, provide for a low-power consumption module arrangement for thesystem 10. In particular, the activation of the GPS receiver 60 once thelocal RTC 62 reaches a predetermined real-time clock time to synchronizea real-time clock time of the local RTC 62 with GPS time reduces theamount of time over which the GPS receiver 60 is active. GPS receiversare known to consume substantial amounts of power when active for longerperiods. Accordingly, activating the GPS receiver 60 only when requiredfor synchronization of the RTC 62 with GPS time provides for substantialreduction in power demand by the system. Managing the change inactivation state of the interruption modules based on the synchronizedGPS time provided to the RTC 60 provides for synchronized interruptionof the cathodic protection system 16 to the metallic structure 14without the requirement for connection to line power or recharging of alocal power source, such as a battery, by external means. The low-powerconsumption module arrangement may include any of the components ormethod steps as described above to provide further low-power consumptionadvantage to the system 10.

While the foregoing description provides what are considered to bepreferred and exemplary embodiments of the present invention, othermodifications of these embodiments also falling within the scope of thepresent invention will be apparent to those skilled in the art.

What is claimed is:
 1. A cathodic protection interruption systemcomprising: a metallic structure embedded in an electrolytic medium; aplurality of passive cathodic protection units embedded in theelectrolytic medium adjacent to and spaced apart along the metallicstructure; a plurality of test units electrically coupled with themetallic structure and each of the plurality of passive cathodicprotection units; and, a low-power consumption component arrangementcomprising: a local real-time clock coupled with each test unit of theplurality of test units and a global positioning system (GPS) receivercoupled with each test unit of the plurality of test units for receivingGPS time from at least one global positioning system satellite in datacommunication therewith; at least one controller communicatively coupledwith each real-time clock and each GPS receiver for activating the GPSreceiver once the local real-time clock reaches a predeterminedreal-time clock time to synchronize a real-time clock time of each localreal-time clock with GPS time; and, a plurality of interruption moduleseach coupled in electrical and data communication with the at least onecontroller, the at least one controller selectively changing anactivation state of each interruption module of the plurality ofinterruption modules once the real-time clock time reaches apredetermined activation state change time to selectively electricallycouple or electrically decouple each passive cathodic protection unit ofthe plurality of passive cathodic protection units from the metallicstructure.
 2. The cathodic protection interruption system according toclaim 1, wherein ones of the passive cathodic protection units of theplurality of passive cathodic protection units are selected from thegroup consisting of bonds and sacrificial anodes.
 3. The cathodicprotection interruption system according to claim 1, further comprising:a plurality of reference electrodes each embedded in the electrolyticmedium proximate to the metallic structure and electrically coupled witha corresponding test unit of the plurality of test units; and, aplurality of voltmeters wherein one voltmeter of the plurality ofvoltmeters is electrically coupled between each reference electrode andcorresponding test unit of the plurality of test units.
 4. The cathodicprotection interruption system according to claim 1, further comprising:a plurality of remote monitoring units each housing a corresponding oneof the at least one interruption modules and in electrical communicationand data communication with a corresponding test unit of the pluralityof test units.
 5. The cathodic protection interruption system accordingto claim 4, wherein each remote monitoring unit of the plurality ofremote monitoring units is configured for wireless cellularcommunication.
 6. The cathodic protection interruption system accordingto claim 4, wherein each remote monitoring unit of the plurality ofremote monitoring units is configured for wireless satellitecommunication.
 7. The cathodic protection interruption system accordingto claim 4, further comprising: a battery serving as a sole power sourcefor at least one of the remote monitoring unit and the correspondingtest station, the battery absent connection with an external powersource.
 8. The cathodic protection interruption system according to oneof claim 6 and claim 7, further comprising: at least one low earth orbitL-band satellite in data communication with each remote monitoring unitof the plurality of remote monitoring units.
 9. The cathodic protectioninterruption system according to claim 1, wherein the GPS receiver isdeactivated after synchronization until the real-time clock reaches thepredetermined real-time clock time.
 10. The cathodic protectioninterruption system according to claim 1, further comprising: at leastone coupon embedded in the electrolytic medium adjacent the metallicstructure and electrically coupled with the at least one cathodicprotection unit via the test station; and, a switch electrically coupledbetween the at least one coupon and the test station for selectivelycoupling and decoupling the at least one coupon from the at least onecathodic protection unit.
 11. The cathodic protection interruptionsystem according to claim 1, wherein the metallic structure is one of apipeline, a marine structure, a bridge, a storage tank, a power linetower, an electrical grid infrastructure component and a coupon.
 12. Thecathodic protection interruption system according to claim 1, whereinthe electrolytic medium is at least one of soil and water.
 13. Thecathodic protection interruption system according to claim 1, furthercomprising: a local power source electrically coupled with at least oneof the test stations and the interruption module.
 14. The cathodicprotection interruption system according to claim 13, wherein the localpower source is a battery absent external augmentation.
 15. The cathodicprotection interruption system according to claim 1, wherein thereal-time clock is a digital temperature-compensated crystal oscillator(DTCXO).
 16. A cathodic protection interruption system comprising: ametallic structure embedded in an electrolytic medium; at least onepassive cathodic protection unit embedded in the electrolytic mediumadjacent to the metallic structure; a test unit electrically coupledwith the metallic structure and the passive cathodic protection unit;and, a low-power consumption component arrangement comprising: a localreal-time clock coupled with the test unit and a global positioningsystem (GPS) receiver coupled with the test unit for receiving GPS timefrom at least one global positioning system satellite in datacommunication therewith; at least one controller communicatively coupledwith the real-time clock and the GPS receiver for activating the GPSreceiver once the local real-time clock reaches a predetermined localtime to synchronize the local real-time clock with GPS time; and, aninterruption module coupled in electrical and data communication withthe at least one controller, the at least one controller selectivelychanging an activation state of the interruption module once thereal-time clock time reaches a predetermined activation state changetime to selectively electrically couple or electrically decouple thepassive cathodic protection unit from the metallic structure.
 17. Thecathodic protection interruption system according to claim 16, whereinthe passive cathodic protection units is selected from the groupconsisting of bonds and sacrificial anodes.
 18. The cathodic protectioninterruption system according to claim 16, further comprising: areference electrode embedded in the electrolytic medium proximate to themetallic structure and electrically coupled with the test unit; and, avoltmeter electrically coupled between the reference electrode and thetest unit.
 19. The cathodic protection interruption system according toclaim 16, further comprising: a remote monitoring unit housing theinterruption module and in electrical communication and datacommunication with the test unit.
 20. The cathodic protectioninterruption system according to claim 19, wherein the remote monitoringunit is configured for wireless cellular communication.
 21. The cathodicprotection interruption system according to claim 19, wherein the remotemonitoring unit is configured for wireless satellite communication. 22.The cathodic protection interruption system according to claim 19,further comprising: a battery serving as a sole power source for atleast one of the test station and the remote monitoring unit, thebattery absent connection with an external power source.
 23. Thecathodic protection interruption system according to one of claim 21 andclaim 22, further comprising: at least one low earth orbit L-bandsatellite in data communication with the remote monitoring unit.
 24. Thecathodic protection interruption system according to claim 16, whereinthe GPS receiver is deactivated after synchronization until thereal-time clock reaches the predetermined real-time clock time.
 25. Thecathodic protection interruption system according to claim 16, furthercomprising: a coupon embedded in the electrolytic medium adjacent themetallic structure and electrically coupled with the passive cathodicprotection unit via the test station; and, a switch electrically coupledbetween the coupon and the test station for selectively coupling anddecoupling the coupon from the passive cathodic protection unit.
 26. Thecathodic protection interruption system according to claim 16, whereinthe metallic structure is one of a pipeline, a marine structure, astorage tank, a bridge, a power line tower, an electrical gridinfrastructure component and a coupon.
 27. The cathodic protectioninterruption system according to claim 16, wherein the electrolyticmedium is at least one of soil and water.
 28. The cathodic protectioninterruption system according to claim 16, further comprising: a localpower source electrically coupled with at least one of the test stationsand the interruption module.
 29. The cathodic protection interruptionsystem according to claim 28, wherein the local power source is abattery absent external augmentation.
 30. The cathodic protectioninterruption system according to claim 16, wherein the real-time clockis a digital temperature-compensated crystal oscillator (DTCXO).
 31. Amethod for changing an activation state of an interruption module forselectively interrupting at least one passive cathodic protection unitfrom a metallic structure, the method comprising the steps of: enablinga global positioning system (GPS) receiver in data communication with acontroller of the interruption module; receiving GPS time via the GPSreceiver from at least one global positioning system satellite in datacommunication therewith; synchronizing a real-time clock time of areal-time clock in data communication with the controller to GPS time;disabling the GPS receiver; and changing the activation state of theinterruption module if a predetermined activation state change time ofthe interruption module is between the local real-time clock time andthe GPS time.
 32. The method according to claim 31 wherein the step ofdisabling the GPS receiver further comprises disabling the GPS receiverfor a predetermined time period.
 33. The method according to claim 31further comprising the step of: enabling the GPS receiver upon expiry ofthe predetermined time period.
 34. The method according to claim 31,wherein the step of synchronizing the real-time clock with GPS timefurther comprises synchronizing the real-time clock with GPS time whenthe real-time clock leads GPS time.
 35. The method according to claim32, wherein the predetermined activation state change time is apredetermined activation time and the interruption module is activatedat the step of changing the activation state.
 36. The method accordingto claim 31, wherein the predetermined activation state change time is apredetermined de-activation time and the interruption module isde-activated at the step of changing the activation state.
 37. Themethod according to claim 31, wherein prior to the step of receiving GPStime via the GPS receiver, the method further comprises the step of:establishing a data communication lock between the GPS receiver and theat least one global positioning system satellite.
 38. The methodaccording to claim 31, wherein the metallic structure is one of apipeline, a marine structure, a storage tank, a bridge, a power linetower, an electrical grid infrastructure component and a coupon.
 39. Themethod according to claim 38, wherein the metallic structure is a couponwhich is embedded in the electrolytic medium adjacent the pipeline andelectrically coupled with the passive cathodic protection unit via aswitch electrically coupled between the coupon and the test station forselectively coupling and decoupling the at least one coupon from thepassive cathodic protection unit.